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Sommaire du brevet 2038100 

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Disponibilité de l'Abrégé et des Revendications

L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Brevet: (11) CA 2038100
(54) Titre français: PROJECTILE NON MORTEL, FRAGILISE
(54) Titre anglais: FRANGIBLE NONLETHAL PROJECTILE
Statut: Périmé
Données bibliographiques
(52) Classification canadienne des brevets (CCB):
  • 102/20
(51) Classification internationale des brevets (CIB):
  • F42B 8/14 (2006.01)
  • F42B 8/16 (2006.01)
  • F42B 12/40 (2006.01)
(72) Inventeurs :
  • LUXTON, DAVID (Canada)
(73) Titulaires :
  • GENERAL DYNAMICS ORDNANCE AND TACTICAL SYSTEMS - CANADA INC. (Canada)
(71) Demandeurs :
  • LUXTON, DAVID (Canada)
(74) Agent: MILTONS IP/P.I.
(74) Co-agent:
(45) Délivré: 2001-05-22
(22) Date de dépôt: 1991-03-12
(41) Mise à la disponibilité du public: 1991-09-13
Requête d'examen: 1998-01-22
Licence disponible: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Non

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
07/491,697 Etats-Unis d'Amérique 1990-03-12

Abrégés

Abrégé anglais




A nonlethal frangible projectile (1) for
delivering fluids and the like to a target is composed of
a soft cap portion (4), and a stronger bass portion (7)
which plugs the rearward end of the cap. Scoring (19)
and a thinned nose region (18) facilitates rupture upon
impact.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.



-6-

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:

1. A two-piece cylindrical projectile (1) for firing
from a firearm by a propellant-charged cartridge, such
projectile (1) comprising:
(a) an aerodynamically shaped thin-walled,
frangible cap portion (4) having:
(i) a closed nose end (12) carrying a
free-flowing filling;
(ii) an open rearward end (8), and
(iii) a surrounding wall (5a) that is sufficiently
strong to sustain loading and firing, but
sufficiently frangible to burst on impact
without causing lethal injury, the wall (5a)
of the cap portion (4) being provided with
multiple longitudinal scoring lines (19)
which close radially at the nose end (12)
wherein the cap wall (5a) is relatively
reduced in thickness with respect to the
wall thickness between the longitudinal
scoring lines (19); and
(b) a plug portion (5) of cylindrical proportions,
sealingly installed arid protruding into the
rearward end (8) of said cap portion (4), said
plug portion (5) being provided with a
cylindrical wall (20) to contain the expansive
effect of propellant gases on firing, and being
provided with an interior cavity (9) within such
cylindrical wall (20), the cavity (9) being of a
dimension that causes the center of mass (10) of
the projectile (1) to be displaced forwardly of
the geometric (11), longitudinal mid-point of the
projectile (1).
2. A projectile (1) as in claim 1 wherein the
scoring lines (19) terminate centrally on said nose end
(12) with a central region (18) of reduced wall
thickness.
3. A projectile (1) as in claim 1 wherein said
scoring lines (19) extend from the nose end of the
projectile towards the rearward end (8), terminating at a
location along the side of said cap portion (4) that does
not over-lie the plug (5).


-7-

4. A projectile as in claim 1, 2 or 3 wherein the
plug (5) is provided with an outer rim (13) that is of a
diameter which will engage with the rifling within a
barrel sized to receive the projectile (1).
5. A projectile (1) as in claim 1, 2 or 3 wherein
said cap (4) and plug (5) are inter-engaged by means of a
complimentary "O" ring type ridge (14) and corresponding
groove (17).

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.





Title: FRANGIBLE NONLETHAL PROJECTILE
FIELD OF THE INVENTION
This invention relates to a new form of nonlethal
projectile and cartridge casing, adapted for use in
05 firearms. More particularly it relates to a frangible
projectile of preferred configuration.
BACKGROUND
In the munitions industry a variety of
projectiles have been proposed for permitting delivery of
a range of chemical agents far various purposes. These
purposes range from marking with a colouring agent, to
selective use of designer chemicals for operational
purposes such as crowd control and special operations.
There have also been various attempts to produce
a frangible projectile for toy guns and for real firearms
but none are known to have overcome satisfactorily all
the problems that may be encountered. Such problems
include:
- stable flight, for accuracy and so the
projectile will hit nose-first;
- sufficient strength to withstand the stress of
feeding and firing in a firearm yet frangible enough to
break upon impact even upon an unrigid surface;
- sufficient sealing so that a filling contained
within the projectile does not leak; and
- imperviousness to environmental extremes of
cold, heat and moisture.
THE INVENTION
The present invention is a two-piece polymer
projectile consisting of an aero dynamically shaped,
thin-shelled, frangible cap, adapted to be filled with a
flowable substance and sealed with a rear plug. It
combines the following features to overcome a number of
the problems normally associated with frangible
projectiles:
(a) the rear plug is relatively rigid in order
to contain the expansive effect of propellant gases;
(b) a recessed compartment in the rear plug
contributes to creating a forward center of gravity for
the projectile; and thereby provide a more stable flight;
(c) the barrel rifling is engaged by the
projectile in the region of the rear plug only, whereby
positive engagement with the barrel rifling imparts spin
without bursting the cap portion of the projectile;
(d) the cap itself is isolated from the rifling



- 2 -
in the gun barrel by dimensioning the cap fractionally
smaller than the gun bore so as to reduce the risk of
rupture which could occur from contact with the rifling;
(e) score lines on the forward portion of the
cap provide separation of the cap release of the filling
on impact;
(f) an indentation region on the nose of the cap
facilitates flexing of the score lines for more rapid and
efficient bursting of the cap on impact;
(g) complete sealing of the filling compound
within the cap is achieved through an integral "O" ring
on the plug which mates with an encircling groove within
the cap for a snap-on sealing fit;
(h) the score lines extending down the side of
the cap do not extend over the plug.
(i) the wall thickness of the cap is selected,
in combination with material selection, to resist
breakage from lateral impact or handling, while remaining
sufficiently frangible on impact so as to be nonlethal.
Preferably the projectile is provided with an
amorphous free-flowing powder, liquid or semi-liquid
filling compound which:
(i) does not significantly change its physical
properties over a temperature range of approximately -20
degrees to plus 50 degrees Celsius; and
(ii) is of sufficient viscosity and/or adherence
to the wall of the projectile cap to prevent the
otherwise destabilizing effect of the compound spinning
at a different rate from the cap.
These and further features of the invention will
be apparent from the description of the preferred
embodiments which now follow.
SUMMARY OF THE FIGURES
Figure 1 - is a transverse sectional view of a cartridge
casing with projectile.
Figure 1a - is an end view of Figure 1.
Figure 2 - is a transverse sectional view of the plug or
base portion of the projectile.
Figure 3 - is a transverse sectional view of the cap or
casing portion of the projectile.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Figure 1 shows a projectile (1), of the type of the
invention, inserted into a cartridge casing (2). The
cartridge casing is provided with a lower energy




- 3 -
propellant means, which may be in the form merely of the
standard percussion cap (3a). Alternately, a lOGJ power
gas--generating propellant (not show) may be provided.
The projectile has a forward cap portion (4) and
a plug portion or plug (5) which serves to plug the open
base region of 'the cap (4). The plug (5) is provided
with an cylindrical portion (6) and a base (7) which
serves as a plate to seal the base of the cad (4).
The base (7) is forward of the rearward end (8)
lU of the plug, providing a cavity (9) therebetween. This
cavity (9) shifts the center of mass (10) of the
projectile (1) forward of its geometric center (11),
midway between the nose (12) of the projectile (1) and
the rearward end (8) of the plug (5). This provides
stability for the projectile (1) in flight.
The plug (5) is preferably made with a wall 5a of
a thickness and of relatively ridged polymeric material
that will burst on impact. Polyethylene has been found
satisfactory. The plug (5) has a cylindrical wall (20)
which serves the function of containing the expansive
forces of expanding propellant gas, and must be
constructed accordingly.
In detail, as shown in Figure (2), the ,plug (5)
may be formed with an outer stiffening annular rim (13).
Further, it may be provided with an annular coupling
ridge (14) capable of providing '°0" ring type sealing
with the cap.
The diameter of the rim (13) may optionally be
such as to provide a tight friction fit with the inner
surface (15) of the casing (2). The diameter of this rim
may also provide a sliding fit with the inner surface of
the barrel of the firearm in which it is to be discharged
(not shown). This will permit the ring (13) to engage
the rifling on the inside of the barrel and impart
longitudinal rotation of the projectile.
The cap (4) is formed of relatively pliable,
resilient material in the form of a thin shell or casing.
The dimensions and material of the cap (4) are such as to
render it susceptible to immediate rupture on impact. A
wall thickness of .025 inches .in polyethylene has been
found satisfactory.
The cap (4) is generally cylindrical with an
aerodynamic, bullet-shaped nose (12). The base region
(16) of the cap (4) makes a tight friction fit with the
cylindrical portion (6) of the body of the plug (5).



- 4 -
Preferably, the inner surface of the cap (5) is provided
with a groove (17) which is complementary to the ridge
(14) on the plug (5). Alternately the ridge (14) and
groove (17) may be reversed.
The outside diameter of the cap (4) when fitted
over the cylindrical portion (16) and ridge (14), as
assembled may, along with the entire cap (5), be of a
smaller diameter than the rim (13). This will reduce the
wear on the cap (5) due to contact with the barrel if the
rim (13) provides a tight sliding fit with the barrel.
Alternately, the cap (7), when placed over the
cylindrical portion (16), optionally by the stretched
fit, may exceed the diameter of the rim (13) sufficiently
to engage the rifling in a barrel and impart longitudinal
rotation to the projectile (1). In either case, the
barrel rifling is positively engaged by the projectile
(1) in the region of the rear plug only.
The cap (4) is provided with narrow longitudinal
strips of thinned cross-section. These "scores" or
scoring lines not cut entirely through the cap (4), but
render it easily burst upon compression by the forces of
impact. At the same time the projectile must be
sufficiently sturdy to sustain loading, and firing,
without bursting. A wall thickness at the scores (17) of
.005 inches in polyethylene has been found satisfactory.
The scores (19), numbering 6 in the preferred
embodiment, are preferably symmetrical positioned about
the axis of the cap (4), closing radially at the nose
(12j to a central region (18) of reduced wall thickness.
This central region (18) is similarly thinned as the
scored regions (19) of the cap (4). Tt covers a
relatively minor portion of the end profile of the cap
(4) at its nose end (12) and is preferably, but
optionally, slightly concave. Its purpose is to
facilitate flexing of the score lines on impact, thus
providing for more rapid and efficient busting of the cap
on impact.
The scores (19) preferably do not extend aver the
region of the "O" ring ridge (14).
The contents of the projectile may include a
powder, gas liquid, semi-liquid or other free-flowing
fluid. The use of such a filling in conjunction with
modest propellant charges, renders the projectile
nonlethal.
Thus, it will be seen from the foregoing that an




- 5 -
improved nonlethal, frangible projectile is provided that
may be fired from a standard firearm.
These and further features of the invention in
its broadest and more narrow aspects are further
described and claimed in the claims which follow.

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , États administratifs , Taxes périodiques et Historique des paiements devraient être consultées.

États administratifs

Titre Date
Date de délivrance prévu 2001-05-22
(22) Dépôt 1991-03-12
(41) Mise à la disponibilité du public 1991-09-13
Requête d'examen 1998-01-22
(45) Délivré 2001-05-22
Expiré 2011-03-12

Historique d'abandonnement

Il n'y a pas d'historique d'abandonnement

Historique des paiements

Type de taxes Anniversaire Échéance Montant payé Date payée
Le dépôt d'une demande de brevet 0,00 $ 1991-03-12
Taxe de maintien en état - Demande - nouvelle loi 2 1993-03-12 100,00 $ 1993-01-29
Enregistrement de documents 0,00 $ 1993-03-09
Taxe de maintien en état - Demande - nouvelle loi 3 1994-03-14 100,00 $ 1994-01-14
Taxe de maintien en état - Demande - nouvelle loi 4 1995-03-13 100,00 $ 1995-02-02
Taxe de maintien en état - Demande - nouvelle loi 5 1996-03-12 150,00 $ 1996-01-18
Taxe de maintien en état - Demande - nouvelle loi 6 1997-03-12 150,00 $ 1997-01-10
Requête d'examen 400,00 $ 1998-01-22
Taxe de maintien en état - Demande - nouvelle loi 7 1998-03-12 150,00 $ 1998-01-22
Taxe de maintien en état - Demande - nouvelle loi 8 1999-03-12 150,00 $ 1998-12-04
Taxe de maintien en état - Demande - nouvelle loi 9 2000-03-13 150,00 $ 2000-01-12
Taxe finale 300,00 $ 2000-10-31
Taxe de maintien en état - Demande - nouvelle loi 10 2001-03-12 200,00 $ 2001-03-07
Taxe de maintien en état - brevet - nouvelle loi 11 2002-03-12 200,00 $ 2002-02-12
Taxe de maintien en état - brevet - nouvelle loi 12 2003-03-12 200,00 $ 2003-02-06
Taxe de maintien en état - brevet - nouvelle loi 13 2004-03-12 250,00 $ 2004-02-03
Taxe de maintien en état - brevet - nouvelle loi 14 2005-03-14 250,00 $ 2005-02-21
Taxe de maintien en état - brevet - nouvelle loi 15 2006-03-13 450,00 $ 2006-03-06
Taxe de maintien en état - brevet - nouvelle loi 16 2007-03-12 450,00 $ 2007-03-05
Enregistrement de documents 100,00 $ 2008-02-08
Taxe de maintien en état - brevet - nouvelle loi 17 2008-03-12 450,00 $ 2008-02-08
Taxe de maintien en état - brevet - nouvelle loi 18 2009-03-12 450,00 $ 2009-02-17
Taxe de maintien en état - brevet - nouvelle loi 19 2010-03-12 450,00 $ 2010-02-18
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
GENERAL DYNAMICS ORDNANCE AND TACTICAL SYSTEMS - CANADA INC.
Titulaires antérieures au dossier
LUXTON, DAVID
SNC INDUSTRIAL TECHNOLOGIES INC./LES TECHNOLOGIES INDUSTRIELLES SNC INC.
SNC TECHNOLOGIES INC.
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
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Description du
Document 
Date
(yyyy-mm-dd) 
Nombre de pages   Taille de l'image (Ko) 
Page couverture 2001-05-02 1 29
Page couverture 1993-12-14 1 16
Abrégé 1993-12-14 1 9
Revendications 1993-12-14 2 57
Dessins 1993-12-14 1 31
Description 1993-12-14 5 227
Dessins représentatifs 1999-07-30 1 12
Dessins représentatifs 2001-05-02 1 12
Taxes 2003-02-06 1 32
Correspondance 2000-10-31 1 35
Cession 2000-10-31 5 143
Poursuite-Amendment 2001-02-06 1 1
Poursuite-Amendment 2001-01-25 3 131
Correspondance 2000-11-06 2 52
Taxes 2000-01-12 1 41
Cession 1991-03-12 8 262
Poursuite-Amendment 1998-01-22 3 126
Taxes 2002-02-12 1 58
Taxes 1998-12-04 1 37
Taxes 1998-01-22 1 42
Taxes 2001-03-07 1 36
Taxes 2004-02-03 1 31
Taxes 2005-02-21 1 30
Taxes 2006-03-06 1 29
Correspondance 2006-10-18 5 177
Taxes 2007-03-05 1 33
Cession 2008-02-08 4 118
Taxes 2008-02-08 1 35
Correspondance 2010-01-21 5 210
Correspondance 2010-02-08 1 13
Correspondance 2010-02-08 1 19
Taxes 1997-01-10 1 45
Taxes 1996-01-18 1 45
Taxes 1995-02-02 1 48
Correspondance 1995-06-02 1 25
Taxes 1995-02-20 1 33
Taxes 1994-01-14 1 37
Taxes 1993-01-29 1 37